Quantcast Fig 7:  Stall Progression Diagram

 

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T-45A/C TS, E2-C2, ADV & IUT Aero-03
Slow-Speed Flight, Stall and Spin, and AOA System
C. Departures
1.
Definition--One wing is producing much more lift
than the other, causing abrupt pitch, roll, and yaw
a.
Aggravated by control inputs
b.
Typically followed by post-stall gyrations
Sg 2, fr 13
2.
Types
Adverse Yaw Departure
NOTE: Asterisked (*) maneuvers are not authorized
in the T-45 syllabus.
a.
Adverse yaw departure*
(1) Entry example:
(a) Simultaneously displace the aileron to
roll the aircraft left while increasing
Overlay 1
back stick pressure to maximum
available
Figure 7: STALL PROGRESSION DIAGRAM
(9-99) Original
Page 3-13


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